The invention discloses a sealing process of a turbine rotor blade cover plate top hole of a gas turbine. The process comprises the steps that (1), top hole pre-processing is conducted; (2), a red copper bar cooperates with the top hole is prepared to be used as a lining; (3), the red copper bar is installed at the bottom of the top hole, sealing alloy powder is delivered into the top hole througha coaxial gas carrying powder delivering device to perform laser cladding process, and the path is single-passage and multi-layer; (4), the red copper bar is separated from the cover plate, and castmodification processing is conducted on the cover plate of which the top hole is sealed; (5), nondestructive examination is conducted on the cover plate on which cast modification is conducted. According to the sealing process, a traditional vacuum brazing process is abandoned, a laser cladding technology is adopted to seal the turbine rotor blade cover plate top hole of the gas turbine, metallurgical bonding is formed between the sealing alloy powder and the top hole inner wall, the bonding strength is high, the bonding does not easily fall in the using process, vacuum does not need to be ensured, the sealing cost is low, and the cladding quality is improved by multi-layer clading.